View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 04384U 70036B 22176.93889437 -.00000016 00000-0 -54523-5 0 9997
2 04384 74.0269 147.8726 0054146 282.0707 140.5713 12.39222808359825
| Epoch (UTC): | 25 June 2022 22:32:00 |
| Eccentricity: | 0.0054146 |
| inclination: | 74.0269° |
| perigee height: | 1467 km |
| apogee height: | 1552 km |
| right ascension of ascending node: | 147.8726° |
| argument of perigee: | 282.0707° |
| revolutions per day: | 12.39222808 |
| mean anomaly at epoch: | 140.5713° |
| orbit number at epoch: | 35982 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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